https://en.wikipedia.org/wiki/Huff-Daland_XB-1
The Huff-Daland XB-1 was a prototype bomber aircraft built for the United States
Army Air Corps.
The XB-1 was the first aircraft named using just a B- designation. Prior to
1926, the U.S. Army used LB- and HB- prefixes, signifying 'Light Bomber' and
'Heavy Bomber'. The first XB-1, called the Super-Cyclops by Huff-Daland, was an
extension of the earlier Huff-Daland XHB-1 'Cyclops'. It was essentially the
same in size, but sported a twin tail and twin engines.
The XB-1's gunnery arrangement was new for an American bomber, but it had been
previously used by the British and the Germans near the end of World War I. The
Army Air Corps had decided that single-engined bombers such as the XHB-1
performed more poorly and with less safety than the more traditional
twin-engined bomber.
Role
Medium bomber
Manufacturer
Huff-Daland Aero Company
First flight
September 1927
Introduction
n/a
Status
Scrapped
Number built
1
Developed from
Huff-Daland XHB-1
The aircraft flew for the first time in September 1927. Its original Packard
engines did not provide enough power for the aircraft, and it was refitted with
more powerful Curtiss Aircraft "Conqueror" engines. This new configuration was
designated the XB-1B.
Three other similar aircraft designs were requested by the Army Air Corps around
the same time which competed against the XB-1 for the contract. Of these three
(the XB-2 Condor, the Sikorsky S-37 and the Fokker XLB-2), the Curtiss model
eventually won, and only a single XB-1 was ever produced.
Specifications (XB-1B)
General characteristics
Crew: 5
Length: 61 ft 6 in (18.7 m)
Wingspan: 85 ft 0 in (25.9 m)
Height: 19 ft 3 in (5.9 m)
Empty weight: 9,462 lb (4,292 kg)
Loaded weight: 16,500 lb (7,480 kg)
(450 kW) each
Performance
Maximum speed: 100 mph (86 kn, 160 km/h)
Range: 700 mi (610 NM, 1,100 km)
Service ceiling: 15,000 ft (4,600 m)
Power/mass: 0.072 hp/lb (120 W/kg)
Armament
Bombs: 2,500 lb (1,100 kg); 4,000 lb (1,800 kg) on short runs
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